- 발사체 충격 방식을 사용한 초음속 액체 제트의 과도 분무 형상에 관한 연구
- ㆍ 저자명
- 신정환,이인철,김희동,구자예,Shin. Jeung-Hwan,Lee. In-Chul,Kim. Heuy-Dong,Koo. Ja-Ye
- ㆍ 간행물명
- 한국액체미립화학회지
- ㆍ 권/호정보
- 2012년|17권 2호|pp.86-93 (8 pages)
- ㆍ 발행정보
- 한국액체미립화학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
The effects of projectile impact system on the transient spray characteristic which is supersonic liquid tip velocity were studied by experimentally. Supersonic liquid jets were generated by impact of a high speed projectile driven by a Two-stage light gas gun. A high speed camera and schlieren optical system were used to capture the spray structures of the supersonic liquid jets. In a case of nozzle assembly Type-A, expansion gases accelerate a projectile which has a mass of 6 grams from 250 m/s at the exit of the launch tube. Accelerated projectile collides with the liquid storage part, then supersonic liquid jets are injected with instantaneous spray tip velocity from 617.78 m/s to 982.54 m/s with various nozzle L/d. However, In a case of nozzle assembly Type-B which has a heavier projectile (60 grams) and lower impact velocity (182 m/s), an impact pressure was decreased. Thus the liquid jet injected at 210 m/s of the maximum velocity did not penetrate a shock wave and fast break-up was occurred. Pulsed injection of liquid column generated second shock wave and multiple shock wave.